Detail publikace

Design of universal control unit for brushless DC motors

Originální název

Design of universal control unit for brushless DC motors

Anglický název

Design of universal control unit for brushless DC motors

Jazyk

en

Originální abstrakt

The paper presents the design of both power and control electronics used to develop a universal BLDC (brushless DC) motor control unit intended for an aircraft fuel metering pump. The controller allows employing various methods for sensor and sensor-less control including frequency, trapezoidal, sinusoidal and fielding oriented control. The power subsystem provides three power totempole switches as well as a wide range of input and auxiliary circuitry. As needed by the target aircraft industry standards, conclusions of a thorough FMECA analysis of the resulting device are given.

Anglický abstrakt

The paper presents the design of both power and control electronics used to develop a universal BLDC (brushless DC) motor control unit intended for an aircraft fuel metering pump. The controller allows employing various methods for sensor and sensor-less control including frequency, trapezoidal, sinusoidal and fielding oriented control. The power subsystem provides three power totempole switches as well as a wide range of input and auxiliary circuitry. As needed by the target aircraft industry standards, conclusions of a thorough FMECA analysis of the resulting device are given.

BibTex


@inproceedings{BUT92775,
  author="Jiří {Toman} and Jan {Hrbáček} and Vladislav {Singule}",
  title="Design of universal control unit for brushless DC motors",
  annote="The paper presents the design of both power and control electronics used to develop a universal BLDC (brushless DC) motor control unit intended for an aircraft fuel metering pump. The controller allows employing various methods for sensor and sensor-less control including frequency, trapezoidal, sinusoidal and fielding oriented control. The power subsystem provides three power totempole switches as well as a wide range of input and auxiliary circuitry. As needed by the target aircraft industry standards, conclusions of a thorough FMECA analysis of the resulting device are given.",
  address="Institute of Theoretical and Applied Mechanics",
  booktitle="Engineering Mechanics 2012, Book of extended abstracts",
  chapter="92775",
  howpublished="print",
  institution="Institute of Theoretical and Applied Mechanics",
  year="2012",
  month="may",
  pages="342--343",
  publisher="Institute of Theoretical and Applied Mechanics",
  type="conference paper"
}